Turbomachine foot unit

ABSTRACT

A turbomachine foot unit with a plurality of feet is provided. The plurality of feet is fastened to a turbomachine. The turbomachine stands upright on a horizontal base. The turbomachine foot includes fastening devices for fastening the feet to the base. At least one of the feet is mounted in a horizontally moveable manner relative to one of the fastening devices fastening the foot to the base.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is the U.S. National Stage of International ApplicationNo. PCT/EP2009/067776 filed Dec. 22, 2009, and claims the benefitthereof. The International Application claims the benefits of GermanPatent Application No. 10 2008 064 371.8 DE filed Dec. 22, 2008. All ofthe applications are incorporated by reference herein in their entirety.

FIELD OF INVENTION

The invention relates to a turbomachine foot unit with a plurality offeet for fastening to a turbomachine and for standing the turbomachineon a horizontal base and with fastening means for fastening the feet tothe base, with the turbomachine fastened on the base at least one of thefeet being mounted so as to be horizontally movable in relation to oneof the fastening means which fastens the foot to the base.

BACKGROUND OF INVENTION

Turbomachines for industrial purposes or in power stations are oftenconnected to an electrical machine, for example a turbocompressor isconnected to an electric motor for driving the turbocompressor or aturbine is connected to a generator for the transmission of force fromthe turbine to the generator. So as not to subject the connecting shaftto excessively high load when force is transmitted between the machines,such a turbomachine is usually fastened on a base, for example afoundation or base frame. The turbomachine rests on this so as to befirmly fixed during operation, the firm fixing also counteractingvibrations of the turbomachine.

To fasten the turbomachine on a base, it is known to place theturbomachine on feet which are screwed firmly to the base. The feet arethemselves connected to the turbomachine, for example welded or cast inone piece with a housing element, so that the turbomachine is firmlyanchored in the base.

EP 1 176286 A1 already discloses a turbocharger with symmetrical longhole fastening. U.S. Pat. No. 4,076,452 A, U.S. Pat. No. 5,108,258 A andWO 98/53183 A1 show turbines with various bearer constructions.

SUMMARY OF INVENTION

An object of the present invention is to specify a turbomachine footunit, by means of which a turbomachine for industrial or power stationuse can be anchored securely to a base.

This object is achieved by means of a turbomachine foot unit of the typeinitially mentioned, in which, according to the invention, with theturbomachine fastened at the base, at least one of the feet is mountedso as to be movable horizontally in relation to one of the fasteningmeans which fastens the foot to the base.

The invention in this case proceeds from the consideration that aturbomachine becomes hot while it is in operation, the heat beingdistributed unevenly in the volume of the turbomachine. For example, inthe case of an air compressor, the air compressed to an increasinglygreater extent from stage to stage becomes warmer, so that theturbomachine is relatively cool at the air inlet and is hot at theoutlet of the compressed air. As a result of the heat, the turbomachineas a whole expands, with the result that stresses and deformations aretransferred to feet fixed firmly to the base. In the case of a frequentchange in temperature of the turbomachine, the feet or the foot unit ofthe turbomachine therefore experience fatigue, and because of thismaterial fatigue is hazardous to secure fastening to the base. Owing tothe movability of at least one of the feet in relation to the horizontalbase or to a fastening means fixed to the base, the corresponding footcan participate in length compensation, so that the mechanical load onthis foot is reduced, as compared with firmly fixed feet.

The base may be a foundation. A base frame, intermediate plate or thelike may also be a base, these then expediently being fastened firmly tothe foundation or ground, that is to say are immovable with respect tothe ground. The feet serve for fastening to the turbomachine and areexpediently fastened, for example welded, to it. In the case of aturbomachine fastened on the base, it is expediently fastened to thebase for the purpose of carrying out its regular operation. Theturbomachine may be a turbocompressor or a turbine and is intended, inparticular, for a power output of at least 100 kW, in particular atleast 500 kW. There may be any number of feet. Four movable feet areadvantageous, more movable feet or, for example, two movable and twoimmovable feet also being conceivable.

Movability is expediently movability along the base. Movability may beone-, two- or three-dimensional movability, although the second and/orthird dimension must not be a horizontal dimension.

In an advantageous embodiment of the invention, at least two of the feetare mounted so as to be horizontally movable independent of one anotherin relation to the fastening means. As a result, they can adapt theirposition especially flexibly even to a complex thermal expansionbehavior of the turbomachine. Independent movability is afforded whenone foot is movable, without forced movement of another footconsequently taking place.

A sliding arrangement, for example of the foot over the base, issufficient for movable mounting. Movability may be facilitated by amovement aid, for example a surface or track which is provided forespecially low-friction sliding of two components one on the other, forexample by an especially smooth surface or a lubricant.

Movability between the movable foot and its fastening means can beachieved in an especially simple way by play between the fastening meansand the feet. Relative movement can take place one-, two- orthree-dimensionally within this play.

Advantageously, the movable foot comprises a foot plate with a recess,through which is led a fastening means which is assigned to the foot andwhich fastens the foot to the base, the foot plate being moved inrelation to the fastening means in the event of horizontal movement ofthe foot. The horizontal size of the recess thus permits the horizontalmovability of the feet. The recess is expediently surrounded completelyby the foot plate. The fastening means may be a screw which is screwedin the base. Its screw head can directly or indirectly fix the footplate vertically.

The fastening means especially advantageously comprises a sleeve with acollar, said sleeve surrounding the screw. The collar can thereby fixthe foot plate vertically, so that, independently of manufacturingaccuracies of the screw, a uniform apportionment of force to the footplate for the purpose of fixing the foot plate can be achieved.

Moreover, the sleeve can limit a pressure force of the screw upon thefoot plate, for example in that said sleeve bears part of the pressureforce of the fastening means on the base. As a result, the clampingforce which the screw exerts on the foot plate, independently of thetightening force of the screw, can be adjusted to a maximum value whichallows horizontal movement of the foot plate over the base, withoutexcessive frictional force having to be overcome. Expediently, thelength of the sleeve as far as the collar is equal to the thickness ofthe foot plate between the base and the collar or a collar support ofthe foot plate.

To facilitate the horizontal movement of the feet, a friction-reducingmeans, for example a viscous lubricant or Teflon, may be introducedbetween the collar and foot plate. The same applies to a connectionbetween a foot plate and a foundation or ground.

In a further advantageous refinement of the invention, the turbomachinefoot unit comprises a fixing means fastened on the base, for fixing partof the turbomachine at a horizontal fixed point against horizontalmovement. The horizontal movement of the turbomachine permitted by thefeet can thereby be restricted, so that, for example, a shaft connectionto an electrical machine is not subjected to excessively high mechanicalloads.

What may be understood as being a horizontal fixed point is a point orlocation, for example on the turbomachine, at which horizontalmovability is prevented. Thus, at the horizontal fixing point, fixingtakes place in all horizontal directions. The fixing means may be ashaped-out portion, for example a bolt, which is fastened to the baseand which engages into a corresponding recess on the turbomachine or onthe foot unit, or vice versa, so that a shaped-out portion on theturbomachine or foot unit engages into a recess fastened to the base.

Expediently, the movable foot and, in particular, all the movable feetare mounted so as to be movable away from the horizontal fixed point andtoward the horizontal fixed point, for example in a star-shaped manner,so that expansion of the turbomachine away from the fixed point can beconverted into a corresponding movement of the feet.

The turbomachine is fixed perpendicularly to the base by means of thefeet. In order to allow thermal expansion, for example in the verticaldirection, the fixing means advantageously allows vertical movement ofthe turbomachine. Overdetermined fixing can thereby be avoided.

The fixing means advantageously lies in a vertical mid-plane which runsthrough a rotor shaft of the fastened turbomachine. A horizontalposition of the shaft of the turbomachine can thereby be fixed, so that,in the event of thermal expansion of the turbomachine, the shaft issubjected to only slight mechanical load. To the same advantage, thefixing means is arranged on a side of the turbomachine which faces adrive, for example an electric motor for driving the turbomachinedesigned as a compressor, or which faces a generator in the case of aturbine.

It is proposed, furthermore, that the turbomachine foot unit comprise aguide means fastened to the base, for restricting the horizontalmovement of part of the turbomachine to one-dimensional movement. Theguide means may be a center guide chock which serves as a radial fixedpoint for preventing a rotation of the turbomachine in the horizontal. Aload on the shaft can be kept low.

For this purpose, the one-dimensional movement is expediently directedin a shaft direction parallel to a rotor shaft of the fastenedturbomachine. Moreover, it is advantageous if the guide means lies in avertical mid-plane which runs through a rotor shaft of the fastenedturbomachine. In order to keep load upon the shaft in the shaftdirection low, in particular at a connection to an electrical machine,it is advantageous if the guide means is arranged on a side of theturbomachine which faces away from the drive.

Moreover, the invention is aimed at a turbomachine with a turbomachinefoot unit, as described above.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention is explained in more detail by means of exemplaryembodiments illustrated in the drawings in which:

FIG. 1 shows a perspective diagrammatic illustration of a turbomachineand of a turbomachine foot unit fastened to it and having four feet,

FIG. 2 shows a fixing diagram in the form of a view of the base fromabove,

FIG. 3 shows a further turbomachine foot unit in a perspective view,

FIG. 4 shows a sectional illustration through a foot of the turbomachinefoot unit from FIG. 3,

FIG. 5 and FIG. 6 show respectively a sectional illustration and a topview of a center guide chock of the turbomachine foot unit from FIG. 3,

FIG. 7 and FIG. 8 show respectively a sectional illustration of the topview of a center guide bolt of the turbomachine foot unit from FIG. 3,and

FIG. 9 shows a turbomachine foot unit on a raised base.

DETAILED DESCRIPTION OF INVENTION

FIG. 1 shows a turbomachine 2 in a diagrammatic perspectiveillustration, with a turbomachine foot unit 4 which is welded to ahousing 16 of the turbomachine 2. The turbomachine foot unit 4 stands ona base 6, indicated in FIG. 1, which extends horizontally and comprisesa planar foundation and, on each foot 8, a foot plate 11. Theturbomachine foot unit 4 comprises four feet 8, each with a foot plate10 and with two foot panels 12, 14 which stand perpendicularly to oneanother and are welded to the housing 16 of the turbomachine 2. The twofoot panels 12, 14 are welded to the foot plate 10 at their end lyingopposite the turbomachine 2. In each case two feet 18 are connected toone another in each case via a transverse panel 18. It is likewiseconceivable that in each case two foot panels 14 and one transversepanel 18 are produced in one piece and the foot panels 12 are in twoparts and are welded to a foot panel 14 on both sides.

Moreover, FIG. 1 illustrates in the manner of an exploded drawing afixing means 20, shown in more detail in FIGS. 7 and 8, and also a guidemeans 22, illustrated in more detail in FIGS. 5 and 6, and, for eachfoot 8, in each case a sleeve 24 which is shown larger in FIG. 4.

FIG. 2 shows a fixing diagram of the turbomachine 2 on the base 6 or itsintermediate plates 11. What are illustrated are four fasteninglocations 26 for the feet 8 on the base 6, a fixing point 30 defined bythe fixing means 20, and a guide region 32 which is defined by the guidemeans 22. Moreover, a dashed line indicates a shaft 34 of a rotor of theturbomachine 2, said shaft being mounted by means of two shaft radialbearings 36 and one shaft axial bearing 38. Also indicated is a coupling40 to a drive, not illustrated, for example an electric motor in thecase of a turbomachine 2 designed as a compressor.

The fixing means 20 is placed vertically below the rotor shaft 34, sothat the latter is arranged in a vertical mid-plane which runsperpendicularly with respect to the paper plane and runs through therotor shaft 34 of the fastened turbomachine 2.

As explained in more detail with reference to the following figures, thefeet 8, in the state fastened on the base 6, are movable in thehorizontal longitudinal direction 42 and horizontal transverse direction44 or only in the horizontal transverse direction 44, so that theyessentially participate in a thermal expansion or contraction movementof the turbomachine 2, and therefore a shear force on the feet 8 or onthe foot panels 12, 14 and their welded joints and also on the fasteningmeans 60 (FIG. 4) remains low. The horizontal longitudinal direction 42is parallel to the longitudinal direction of the rotor shaft 34 of theturbomachine and the horizontal transverse direction 44 is transverse tothe longitudinal direction of the rotor shaft 34.

By the fixing means 20, the turbomachine 2 is fixed, on its side facingthe coupling 40, at the bottom at the fixing point 30 in all horizontaldirections 42, 44, so that movement of the turbomachine 2 in allhorizontal directions 42, 44 is prevented there. However, movementperpendicular to the horizontal directions 42, 44, that is to sayperpendicularly to the base 6, is possible, so that the turbomachine 2can participate in thermal expansion of the foot panels 12, 14 withoutstresses.

When the turbomachine 2 is in operation, it heats up, and therefore itshousing 16 expands thermally. Expansion takes place in all three spatialdirections. Since the turbomachine 2 is held by the turbomachine footunit 4 from below only, the fixing of the turbomachine 2 on the base 6generates no mechanical stresses in the turbomachine 2 in the verticaldirection or perpendicularly to the base. However, as a result of theexpansion of the turbomachine 2 in the horizontal directions 42, 44,stresses would act upon the feet 8 if these were fixed firmly to thebase 6.

With only the horizontal directions 42, 44 being considered, theturbomachine 2 is fixed at the fixing point 30 by the fixing means 20.This point on the turbomachine 2 is therefore stationary during allhorizontal expansion movements. This is contrary to the feet 8 which arepushed away from the fixing point 30 as a result of thermal expansion ofthe turbomachine 2. The two feet 8 adjacent to the fixing means 20therefore move away from the fixing point 30 in the horizontaltransverse direction 44 and, in the event of thermal contraction, towardthe fixing point 30. The two feet 8 located further away move about thefastening location 26 both in the horizontal longitudinal direction 42and in the horizontal transverse direction 44. The guide means 22prevents movement of the turbomachine 2 in the guide region 32 in thehorizontal transverse direction 44 and permits only the movement in thehorizontal longitudinal direction 42. As a result, a rotational movementof the turbomachine 2 about the fixing point 30 is prevented andtherefore the mechanical load on the shaft 34 or coupling 40 is keptlow.

FIG. 3 shows an alternative turbomachine foot unit 52, without aturbomachine 2 placed on it, in a perspective illustration. Thedescription of the following figures is restricted essentially to thedifferences with respect to the exemplary embodiment from FIG. 1, towhich reference is made with regard to features and functions whichremain the same. Components which essentially remain the same arebasically designated by the same reference symbols and features notmentioned are adopted in the following exemplary embodiments, withoutbeing described again.

In contrast to the turbomachine foot unit 4, the turbomachine foot unit52 comprises foot panels 54 connecting two feet 8 to one another, andcontinuous transverse panels 56 which at their two outer ends likewiseform foot panels welded to the foot panels 54. The foot panels 54 andtransverse panels 56 are themselves welded to the feet 8.

In FIG. 3, recesses 58 in the foot plates 10 can be seen, which are setup in FIG. 4 in a sectional view. The sleeves 24 are inserted into theserecesses 58 for fastening the turbomachine foot unit 52 on the base 6,the fastening means 60 designed in each case as a screw being ledthrough said sleeves. The fastening means 60 is screwed to the base 6and thus presses the sleeve 24 onto the base 6. The pressure force mayin this case be low. It is important merely to have fixing in thevertical direction.

The sleeve 24 comprises at its outer end a collar 62 which, on the onehand, forms a support for the screw head and, on the other hand,partially covers a shoulder 64 of the recess 58 and therefore liesinside the recess 58 on the foot plate 10. The length 66 of the sleeve24 from its lower end as far as the collar 62 is in this case selectedsuch that it is equal to the thickness of the foot plate 10 from thebase 6 as far as the shoulder 64. By the sleeve 24 being braced on thebase 6, the foot plate 10 is also thus secured against movement in thevertical direction 68 away from the base 6. However, the foot plate 10is free in terms of its movement in the horizontal directions 42, 44,insofar as the recess 58 is larger in its diameter by double the length70 than the diameter of the sleeve 24 in its lower region or in theregion of the collar 62. By virtue of this play, all the foot plates 10can be moved in both horizontal directions 42, 44 and in all horizontaldirections lying between them, the feet 8 being horizontally movableindependent of one another.

In this case, only the friction of the foot plate 10 on the base 6 andbetween the foot plate 10 and the collar 62 has to be overcome. Toreduce this friction, a lubricant 72 in the form of a Teflon ring orTeflon film is introduced between the collar 62 and the shoulder 64 ofthe foot plate 10. If the fastening means 60 fastens a foot 8 only to anintermediate plate 11 of the base 6 and horizontal movement between theintermediate plate 11 and foundation or ground is possible, thelubricant may be arranged between the intermediate plate 11 and groundor, in general, between two elements movable horizontally with respectto one another, one being fastened to the foot 8 and the other to thebase 6.

FIG. 5 shows a guide means 22 in the view in horizontal longitudinaldirection 42 and FIG. 6 shows a top view of that part of the guide means22 which is fastened on the base 6. A guide chock 76 is welded on a baseplate 74 screwed to the base 6 or the intermediate plate 11 and has ashaped-out portion 78 which is of elongate form in the horizontallongitudinal direction 42. A guide 80 welded to the housing 16 bears onboth sides in the horizontal transverse direction 44 against thisshaped-out portion 78 which forms a kind of guide rail, so that theguide 80 and, with it, the turbomachine 2 are prevented from movement inthe horizontal transverse direction 44 in the guide region 32. Movementin the horizontal longitudinal direction 42 is guided by the rail-likeshaped-out portion 78.

Similarly to FIGS. 5 and 6, FIGS. 7 and 8 show the fixing means 20 in alateral illustration and in a top view. A bolt 82 is plugged into arecess in a guide 84 on the housing 16 and thus blocks movement of theturbomachine 2 at the fixing point 30 in all horizontal directions 42,44. However, as in the case of the guide means 22, movement in thevertical direction 68 is maintained. Although rotational movement of theturbomachine 2 about the fixing point 30 is not blocked by the fixingmeans 20 on account of the rotationally symmetrical design of the bolt72 and recess in the guide 84, this rotational movement is neverthelessblocked by the guide means 22, as described.

FIG. 9 shows a further exemplary embodiment having a turbomachine footunit 86 with feet 88 in which a horizontal sliding plane between a foot88 and a base 6 lies vertically level with a shaft of the turbomachine.For this purpose, the base comprises chocks 90 which raise the base 6 tothis sliding plane and which can be stiffened in a stable manner withrespect to one another in the horizontal direction. Center guidance bythe fixing means 20 and guide means 22 is maintained. However, thermalexpansion not only causes movement of the components of the turbomachineupward, but also uniformly upward from the machine axis, which lies inthe middle of the machine shaft, and downward away from the feet 88 orthe sliding plane between the feet 88 and base 6. The machine shafttherefore remains in its position, both vertically and horizontally, andno appreciable error of alignment occurs due to thermal expansion.

1.-12. (canceled)
 13. A turbomachine foot unit, comprising: a pluralityof feet being fastened to a turbomachine, the turbomachine standing on ahorizontal base; a plurality of fastening devices for fastening theplurality of feet on the horizontal base, wherein at least one of thefeet is mounted so as to be horizontally movable in relation to one ofthe fastening devices which fastens the at least one of the feet to thebase; a fixing device, fastened to the base, for fixing the turbomachineat a horizontal fixed point against horizontal movement; and a guidedevice, fastened to the base, for restricting the horizontal movement ofthe turbomachine to a one-dimensional movement, wherein theone-dimensional movement is directed in a direction parallel to a rotorshaft of the turbomachine.
 14. The turbomachine foot unit as claimed inclaim 13, wherein at least two of the feet are mounted so as to behorizontally movable independently of one another in relation to thefastening devices.
 15. The turbomachine foot unit as claimed in claim13, wherein the at least one movable foot has a foot plate with arecess, wherein the fastening device fastening the foot to the base isled through the recess, and wherein the foot plate is moved in relationto the fastening device when the foot horizontally moves.
 16. Theturbomachine foot unit as claimed in claim 15, wherein each fasteningdevice comprises a screw which is led through a sleeve having a collarand which is screwed to the base, the collar pressing the foot plateonto the base.
 17. The turbomachine foot unit as claimed in claim 16,wherein the sleeve bears part of a pressure force of the fasteningdevice onto the base.
 18. The turbomachine foot unit as claimed in claim16, wherein a friction-reducing device is introduced between the collarand foot plate.
 19. The turbomachine foot unit as claimed in claim 17,wherein a friction-reducing device is introduced between the collar andfoot plate.
 20. The turbomachine foot unit as claimed in claim 13,wherein the movable foot is mounted so as to be movable away from thehorizontal fixed point and toward the horizontal fixed point.
 21. Theturbomachine foot unit as claimed in claim 13, wherein the fixing devicepermits vertical movement of the turbomachine.
 22. The turbomachine footunit as claimed in claim 13, wherein the fixing device lies in avertical mid-plane which runs through the rotor shaft of theturbomachine.
 23. The turbomachine foot unit as claimed in claim 13,wherein the fixing device is arranged on a side of the turbomachinewhich faces a drive.
 24. The turbomachine foot unit as claimed in claim13, wherein the guide device lies in a vertical mid-plane which runsthrough the rotor shaft of the turbomachine.
 25. The turbomachine footunit as claimed in claim 13, wherein the guide device is arranged on aside of the turbomachine which faces away from a drive.